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GOE 227 (MVA H.37) AIRFOIL (goe227-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 227 (MVA H.37) AIRFOIL (goe227-il)
Reynolds number: 1,000,000
Max Cl/Cd: 134.76 at α=2°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe227-il-1000000-n5.txt
Download as CSV file: xf-goe227-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 227 (MVA H.37) AIRFOIL                      
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.5649   0.05438   0.05121  -0.1233   0.7982   0.0250
 -13.250  -0.6128   0.04075   0.03735  -0.1397   0.7912   0.0250
 -13.000  -0.6045   0.03293   0.02930  -0.1545   0.7848   0.0253
 -12.750  -0.5778   0.02762   0.02381  -0.1664   0.7793   0.0257
 -12.500  -0.5439   0.02377   0.01979  -0.1760   0.7722   0.0261
 -12.250  -0.5065   0.02087   0.01668  -0.1842   0.7651   0.0265
 -12.000  -0.4723   0.01929   0.01493  -0.1887   0.7561   0.0268
 -11.750  -0.4408   0.01836   0.01385  -0.1913   0.7458   0.0270
 -11.500  -0.4085   0.01717   0.01250  -0.1945   0.7309   0.0276
 -11.250  -0.3776   0.01637   0.01153  -0.1965   0.7070   0.0280
 -11.000  -0.3477   0.01580   0.01078  -0.1980   0.6810   0.0285
 -10.750  -0.3176   0.01533   0.01017  -0.1993   0.6642   0.0289
 -10.500  -0.2873   0.01490   0.00962  -0.2004   0.6531   0.0294
 -10.250  -0.2567   0.01447   0.00910  -0.2016   0.6464   0.0299
 -10.000  -0.2261   0.01407   0.00859  -0.2026   0.6409   0.0303
  -9.500  -0.1647   0.01335   0.00769  -0.2046   0.6329   0.0311
  -9.250  -0.1340   0.01302   0.00729  -0.2055   0.6300   0.0314
  -9.000  -0.1031   0.01269   0.00688  -0.2064   0.6273   0.0318
  -8.750  -0.0721   0.01231   0.00645  -0.2074   0.6247   0.0326
  -8.500  -0.0413   0.01202   0.00611  -0.2082   0.6223   0.0333
  -8.250  -0.0107   0.01178   0.00581  -0.2090   0.6200   0.0341
  -7.750   0.0505   0.01134   0.00528  -0.2103   0.6163   0.0357
  -7.500   0.0812   0.01114   0.00503  -0.2110   0.6150   0.0364
  -7.250   0.1120   0.01092   0.00477  -0.2117   0.6137   0.0373
  -7.000   0.1428   0.01071   0.00454  -0.2124   0.6124   0.0386
  -6.750   0.1734   0.01054   0.00435  -0.2130   0.6110   0.0399
  -6.500   0.2039   0.01039   0.00416  -0.2136   0.6097   0.0413
  -6.250   0.2343   0.01026   0.00400  -0.2141   0.6082   0.0425
  -6.000   0.2648   0.01012   0.00383  -0.2147   0.6062   0.0444
  -5.750   0.2949   0.01002   0.00371  -0.2152   0.6036   0.0465
  -5.500   0.3249   0.00995   0.00360  -0.2156   0.6008   0.0485
  -5.250   0.3552   0.00986   0.00348  -0.2161   0.5989   0.0503
  -5.000   0.3856   0.00975   0.00338  -0.2167   0.5978   0.0525
  -4.750   0.4159   0.00966   0.00329  -0.2171   0.5964   0.0546
  -4.500   0.4461   0.00959   0.00319  -0.2176   0.5946   0.0563
  -4.250   0.4763   0.00950   0.00309  -0.2181   0.5925   0.0581
  -4.000   0.5065   0.00943   0.00302  -0.2185   0.5908   0.0604
  -3.750   0.5365   0.00938   0.00296  -0.2189   0.5891   0.0626
  -3.500   0.5663   0.00935   0.00291  -0.2193   0.5874   0.0646
  -3.250   0.5960   0.00933   0.00286  -0.2196   0.5858   0.0658
  -3.000   0.6260   0.00927   0.00279  -0.2201   0.5842   0.0681
  -2.750   0.6557   0.00924   0.00275  -0.2205   0.5822   0.0707
  -2.500   0.6857   0.00919   0.00271  -0.2209   0.5807   0.0734
  -2.250   0.7157   0.00915   0.00267  -0.2213   0.5792   0.0752
  -2.000   0.7455   0.00913   0.00264  -0.2216   0.5778   0.0765
  -1.750   0.7755   0.00907   0.00259  -0.2221   0.5763   0.0797
  -1.500   0.8053   0.00903   0.00256  -0.2225   0.5745   0.0828
  -1.250   0.8349   0.00901   0.00254  -0.2228   0.5721   0.0861
  -1.000   0.8643   0.00900   0.00253  -0.2231   0.5693   0.0897
  -0.750   0.8936   0.00900   0.00253  -0.2234   0.5665   0.0970
  -0.500   0.9230   0.00899   0.00254  -0.2238   0.5644   0.1078
  -0.250   0.9528   0.00894   0.00255  -0.2242   0.5626   0.1243
   0.000   0.9825   0.00890   0.00256  -0.2246   0.5597   0.1395
   0.250   1.0119   0.00888   0.00257  -0.2249   0.5559   0.1523
   0.500   1.0411   0.00886   0.00258  -0.2253   0.5520   0.1709
   0.750   1.0709   0.00874   0.00264  -0.2259   0.5484   0.2597
   1.000   1.1001   0.00874   0.00270  -0.2262   0.5452   0.2798
   1.250   1.1290   0.00876   0.00276  -0.2264   0.5403   0.2945
   1.500   1.1572   0.00882   0.00282  -0.2265   0.5335   0.3046
   1.750   1.1855   0.00889   0.00288  -0.2266   0.5252   0.3118
   2.000   1.2128   0.00900   0.00295  -0.2265   0.5106   0.3192
   2.250   1.2377   0.00928   0.00309  -0.2261   0.4815   0.3250
   2.500   1.2605   0.00972   0.00335  -0.2252   0.4500   0.3315
   2.750   1.2842   0.01009   0.00363  -0.2246   0.4283   0.3409
   3.000   1.3087   0.01041   0.00387  -0.2241   0.4130   0.3482
   3.250   1.3335   0.01068   0.00411  -0.2236   0.4017   0.3565
   3.500   1.3592   0.01088   0.00430  -0.2233   0.3938   0.3649
   3.750   1.3845   0.01111   0.00450  -0.2229   0.3874   0.3712
   4.000   1.4107   0.01125   0.00467  -0.2227   0.3823   0.3807
   4.250   1.4361   0.01144   0.00488  -0.2224   0.3763   0.3937
   4.500   1.4607   0.01166   0.00511  -0.2219   0.3705   0.4100
   4.750   1.4866   0.01180   0.00530  -0.2216   0.3668   0.4254
   5.250   1.5361   0.01218   0.00574  -0.2208   0.3577   0.4595
   5.500   1.5597   0.01241   0.00600  -0.2201   0.3524   0.4797
   5.750   1.5839   0.01260   0.00624  -0.2196   0.3470   0.5009
   6.000   1.6059   0.01289   0.00654  -0.2186   0.3396   0.5200
   6.250   1.6277   0.01318   0.00683  -0.2177   0.3319   0.5364
   6.500   1.6484   0.01348   0.00714  -0.2165   0.3246   0.5506
   6.750   1.6665   0.01381   0.00747  -0.2148   0.3177   0.5636
   7.000   1.6829   0.01417   0.00783  -0.2128   0.3085   0.5762
   7.250   1.6995   0.01461   0.00827  -0.2110   0.2984   0.5894
   7.500   1.7151   0.01513   0.00877  -0.2091   0.2881   0.6031
   7.750   1.7332   0.01554   0.00921  -0.2076   0.2804   0.6198
   8.000   1.7477   0.01614   0.00982  -0.2056   0.2699   0.6436
   8.250   1.7600   0.01683   0.01066  -0.2034   0.2531   0.7758
   8.500   1.7642   0.01760   0.01158  -0.1998   0.2333   1.0000
   8.750   1.7695   0.01882   0.01270  -0.1967   0.2137   1.0000
   9.000   1.7714   0.02034   0.01409  -0.1932   0.1905   1.0000
   9.250   1.7547   0.02320   0.01667  -0.1877   0.1453   1.0000
   9.500   1.7509   0.02536   0.01871  -0.1842   0.1217   1.0000
   9.750   1.7544   0.02709   0.02039  -0.1816   0.1088   1.0000
  10.000   1.7586   0.02882   0.02208  -0.1793   0.0975   1.0000
  10.250   1.7467   0.03187   0.02496  -0.1754   0.0658   1.0000
  10.500   1.7292   0.03557   0.02853  -0.1714   0.0346   1.0000
  10.750   1.7318   0.03765   0.03061  -0.1693   0.0276   1.0000
  11.000   1.7373   0.03953   0.03252  -0.1676   0.0240   1.0000
  11.250   1.7424   0.04151   0.03452  -0.1660   0.0212   1.0000
  11.500   1.7489   0.04340   0.03645  -0.1646   0.0194   1.0000
  11.750   1.7542   0.04542   0.03850  -0.1631   0.0178   1.0000
  12.000   1.7599   0.04747   0.04059  -0.1618   0.0166   1.0000
  12.250   1.7653   0.04959   0.04275  -0.1606   0.0156   1.0000
  12.500   1.7702   0.05180   0.04501  -0.1594   0.0148   1.0000
  12.750   1.7744   0.05413   0.04737  -0.1582   0.0140   1.0000
  13.000   1.7788   0.05644   0.04975  -0.1571   0.0135   1.0000
  13.250   1.7831   0.05880   0.05216  -0.1561   0.0131   1.0000
  13.500   1.7870   0.06121   0.05463  -0.1550   0.0126   1.0000
  13.750   1.7896   0.06382   0.05729  -0.1540   0.0122   1.0000
  14.000   1.7917   0.06648   0.06000  -0.1531   0.0117   1.0000
  14.250   1.7925   0.06932   0.06289  -0.1521   0.0113   1.0000
  14.500   1.7927   0.07223   0.06587  -0.1512   0.0109   1.0000
  14.750   1.7947   0.07493   0.06863  -0.1503   0.0107   1.0000
  15.000   1.7954   0.07784   0.07161  -0.1495   0.0104   1.0000
  15.250   1.7960   0.08076   0.07460  -0.1488   0.0101   1.0000
  15.500   1.7952   0.08391   0.07782  -0.1481   0.0098   1.0000
  15.750   1.7945   0.08702   0.08098  -0.1475   0.0096   1.0000
  16.000   1.7919   0.09043   0.08447  -0.1469   0.0093   1.0000
  16.250   1.7902   0.09375   0.08785  -0.1464   0.0091   1.0000
  16.500   1.7861   0.09746   0.09164  -0.1460   0.0089   1.0000
  16.750   1.7819   0.10122   0.09547  -0.1457   0.0086   1.0000
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